US3942362A - Roof truss testing machine - Google Patents
Roof truss testing machine Download PDFInfo
- Publication number
- US3942362A US3942362A US05/496,528 US49652874A US3942362A US 3942362 A US3942362 A US 3942362A US 49652874 A US49652874 A US 49652874A US 3942362 A US3942362 A US 3942362A
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- US
- United States
- Prior art keywords
- truss
- tube
- machine
- deflection
- flange
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000012360 testing method Methods 0.000 title claims abstract description 27
- 230000001105 regulatory effect Effects 0.000 claims description 6
- 230000006378 damage Effects 0.000 claims description 2
- 238000013461 design Methods 0.000 description 2
- 230000001066 destructive effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000009658 destructive testing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
- 238000012956 testing procedure Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0041—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress
- G01M5/005—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress by means of external apparatus, e.g. test benches or portable test systems
Definitions
- This invention relates to a machine for testing trusses, particularly for buildings and mobile homes which require a large number of identical roof trusses.
- Objects of the invention are, therefore, to provide a truss testing machine, to provide a machine for applying a simulated snow load on a roof truss, and to provide a machine of the type described which is relatively simple and inexpensive to build and which gives thoroughly accurate and reliable results in operation.
- the present machine provides means for quickly and accurately testing a complete truss without regard to the numerous details which have heretofore been considered, such as theoretical design, quality of the wood, strength of the grip plate connections and other such features and characteristics.
- the present machine applies a simple load test under which the truss either passes or fails. If the truss passes the test, it may be used; if it fails, it is rejected and destroyed.
- the present testing machine comprises a table having an upstanding flange along one side.
- a truss to be tested is laid flat on the table with a load cell interposed between one end of the bottom chord of the truss and the table flange and a block interposed between the opposite end of the bottom chord and the table flange.
- a flattened flexible tube is disposed on edge along a similar flange on the opposite side of the table. Blocks are inserted between the flexible tube and the top chord to simulate a uniform snow load when the tube is inflated. One-half the total load is measured directly by the load cell and the deflection of the center of the bottom chord is measured by a scale on the table. If the truss successfully passes the loading test, this fact is registered by a rubber stamp activated by an automatic mechanism.
- This testing procedure is based on the existence of a recognized relationship between the amount of deflection occurring in a short loading interval and the amount of deflection occurring after a long interval, such as days, weeks or months. This makes if possible to determine in a few seconds how a structure will behave under a continuous load existing for any specified length of time, as for example, a snow load persisting through the winter months.
- FIG. 1 is a top plan view of a machine embodying the invention
- FIG. 2 is a view on the line 2--2 in FIG. 1;
- FIG. 3 is a view showing the pneumatic system
- FIG. 4 is a wiring diagram of the electrical system
- FIG. 5 is a schematic diagram of the machine functions.
- the truss T to be tested has a bottom chord 10, a top chord 11 and web members 12, all held together by conventional spiked grip plates 13.
- the truss T is laid flad on a support member 14, such as a layer of slats, on a horizontal table 15 which has an upstanding abutment flange 20 extending along one side thereof.
- Bottom chord 10 is arranged parallel with flange 20 and a block 21 is inserted between one end of chord 10 and the flange 20.
- a conventional load cell 22 is inserted between the opposite end of chord 10 and flange 20.
- Load cell 22 has a piston 23 arranged to engage the chord 10. Piston 23 operates in a hydraulic cylinder to actuate a pressure gauge 24, which is calibrated to indicate the number of pounds of load applied to the piston. The movement of the piston under load is insignificant in relation to the amount of deflection to be measured in the center of the truss.
- a flattened flexible tube such as a fire hose 25 is disposed on edge against an upstanding abutment flange 26 which is parallel with the flange 20.
- the opposite ends of tube 25 are closed and sealed by a suitable means such as clamps 27.
- a series of blocks 30 is inserted between tube 25 and top chord 11 along the entire length of the top chord with the blocks in substantially edge to edge relationship.
- Each block 30 has one end 31 cut off square to abut the flattened tube 25 and the other end 32 cut off on an angle corresponding to the angle of top chord 11.
- a circular saw 36 mounted on table 15 is swung down into position to cut off square ends on the chord members 10 and 11. Useless sawing operations are thereby avoided on trusses which fail to pass the test and on trusses which are tested to destruction.
- Slat support 14 elevates the truss to the level of the center of flattened tube 25 and holds the truss above the table for the operation of saw 36.
- the air is evacuated from tube 25, collapsing the tube and allowing the blocks 30 to be pushed back so that the truss may be removed from table 15 and a new truss placed in position for testing.
- the pneumatic system in FIG. 3 is supplied by a pressure line 40 and vacuum line 41.
- One branch of pressure line 40 is connected to a pressure regulating valve 42 which may be adjusted to supply break load pressure to tube 25.
- a second branch of pressure line 40 is connected to a pressure regulating valve 43 which may be adjusted to produce a pre-determined loading on load cell scale 24 for deflection testing.
- the break load air pressure is indicated on a pressure gauge 44 and the deflection load air pressure is indicated on a pressure gauge 45.
- a three-position manual selector valve 46 is arranged to connect the supply pipe 47 for tube 25 to pipe 48 for admitting break load pressure, to pipe 49 for admitting deflection load pressure and to vacuum line 41 for exhausting the air from tube 25 after the test.
- a deflection testing program for each truss is controlled by the electrical system shown in FIG. 4.
- manual valve 46 is turned to connect tube 25 with pressure pipe 49.
- manual switch 55 is closed on contact 56
- ten second timer relay TR is energized, causing the relay to close its normally open contacts TR 1 and open its normally closed contacts TR 2 .
- the closing of contacts TR 1 energizes the coil of solenoid valve SV 1 to inflate tube 25 and load the truss.
- the inflation pressure has previously been adjusted by regulating valve 43 to a value which will produce a prescribed loading on the load cell scale 24.
- timing relay TR deenergizes itself by means of an internal switch (not shown), causing closed relay contacts TR 1 to re-open and causing the opened contacts TR 2 to re-close.
- the opening of contacts TR 1 deenergizes solenoid valve SV 1 to close the valve and shut off air pressure to tube 25.
- the air is evacuated from tube 25 by turning manual valve 46 to connect the tube with vacuum line 41.
- the re-closing of timer relay contacts TR 2 energizes solenoid valve SV 2 to open the valve and admit air to stamp cylinder 57 in FIG. 1 to actuate the rubber stamp 58.
- Stamp 58 applies some word or symbol to the truss, indicating passing of the test and acceptance.
- switch 55 is opened and the truss is replaced with the next truss to be tested.
- the opening of switch 55 re-sets the timer relay TR.
- manual valve 46 When the next truss is placed on the table for testing, manual valve 46 is turned to connect tube 25 with pressure pipe 49 and switch 55 is closed on contact 56 as before, energizing timing relay TR for a ten second interval.
- the energizing of relay TR opens the closed contacts TR 2 and closes the open contacts TR 1 to energize solenoid valve SV 1 and admit the predetermined air pressure into tube 25 to load the truss for a ten second interval. Let it be assumed that this truss does not pass the test. In this event, excessive deflection of the truss closes the limit switch 60, energizing relay R and truss fail light 61.
- relay R closes normally open relay contacts R 1 and opens normally closed relay contacts R 2 .
- Contacts R 1 close a holding circuit for relay coil R and truss fail light 61 so that these elements remain energized even if switch 60 opens during or after the ten second load period.
- contacts TR 2 close but the contacts R 2 remain open, causing solenoid valve SV 2 to remain deenergized and the rubber stamp 58 is not actuated. This truss is, therefore, rejected.
- Timing relay TR deenergizes itself as before and opens contacts TR 1 . Solenoid valve SV 1 is thereby also deenergized to close valve SV 1 in FIG. 3 and permit deflation of tube 25 by manual selector valve 46. After completion of the test switch 55 is opened, causing timer relay TR to re-set.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
Description
Claims (14)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/496,528 US3942362A (en) | 1974-08-12 | 1974-08-12 | Roof truss testing machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/496,528 US3942362A (en) | 1974-08-12 | 1974-08-12 | Roof truss testing machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3942362A true US3942362A (en) | 1976-03-09 |
Family
ID=23973032
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US05/496,528 Expired - Lifetime US3942362A (en) | 1974-08-12 | 1974-08-12 | Roof truss testing machine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3942362A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5412995A (en) * | 1994-06-10 | 1995-05-09 | Factory Mutual Research Corporation | Single-ply roof cover fatigue tester |
| US6035715A (en) * | 1997-09-15 | 2000-03-14 | Entela, Inc, | Method and apparatus for optimizing the design of a product |
| US6247366B1 (en) | 1997-09-15 | 2001-06-19 | Alexander J. Porter | Design maturity algorithm |
| US20030163269A1 (en) * | 1997-09-15 | 2003-08-28 | Porter Alexander J. | Control system for a failure mode testing system |
| CN100416257C (en) * | 2003-04-26 | 2008-09-03 | 陈东兆 | Loading system suitable for space structure to carry out bearing strength test in vertical direction |
| US7587946B2 (en) | 2006-08-31 | 2009-09-15 | Tunney Timothy T | Method and apparatus for testing roof edge components |
| US20140090479A1 (en) * | 2012-09-28 | 2014-04-03 | Airbus Operations Gmbh | Test method, test rigs and control system |
| CN110595901A (en) * | 2019-09-29 | 2019-12-20 | 扬州大学 | A new truss joint self-balancing test device and its test method |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2058444A (en) * | 1933-04-19 | 1936-10-27 | Harrison Lloyd | Beam testing device |
| US2668444A (en) * | 1950-03-31 | 1954-02-09 | Berman Morris | Stress determining instrument |
| US3158021A (en) * | 1961-02-06 | 1964-11-24 | Western Pine Ass | Lumber testing apparatus |
| US3512404A (en) * | 1968-08-08 | 1970-05-19 | Automated Building Components | Truss testing method and apparatus |
-
1974
- 1974-08-12 US US05/496,528 patent/US3942362A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2058444A (en) * | 1933-04-19 | 1936-10-27 | Harrison Lloyd | Beam testing device |
| US2668444A (en) * | 1950-03-31 | 1954-02-09 | Berman Morris | Stress determining instrument |
| US3158021A (en) * | 1961-02-06 | 1964-11-24 | Western Pine Ass | Lumber testing apparatus |
| US3512404A (en) * | 1968-08-08 | 1970-05-19 | Automated Building Components | Truss testing method and apparatus |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5412995A (en) * | 1994-06-10 | 1995-05-09 | Factory Mutual Research Corporation | Single-ply roof cover fatigue tester |
| US6035715A (en) * | 1997-09-15 | 2000-03-14 | Entela, Inc, | Method and apparatus for optimizing the design of a product |
| US6247366B1 (en) | 1997-09-15 | 2001-06-19 | Alexander J. Porter | Design maturity algorithm |
| US20030163269A1 (en) * | 1997-09-15 | 2003-08-28 | Porter Alexander J. | Control system for a failure mode testing system |
| US20050049807A1 (en) * | 1997-09-15 | 2005-03-03 | Porter Alexander J. | Control system for a failure mode testing system |
| US7024323B2 (en) | 1997-09-15 | 2006-04-04 | Entela, Inc. | Control system for a failure mode testing system |
| US20060161398A1 (en) * | 1997-09-15 | 2006-07-20 | Porter Alexander J | Control system for a failure mode testing system |
| US7136769B2 (en) | 1997-09-15 | 2006-11-14 | Entela, Inc. | Control system for a failure mode testing system |
| US20070061095A1 (en) * | 1997-09-15 | 2007-03-15 | Porter Alexander J | Control system for a failure mode testing system |
| US7260492B2 (en) | 1997-09-15 | 2007-08-21 | Intertek Etl Entela | Control system for a failure mode testing system |
| CN100416257C (en) * | 2003-04-26 | 2008-09-03 | 陈东兆 | Loading system suitable for space structure to carry out bearing strength test in vertical direction |
| US7587946B2 (en) | 2006-08-31 | 2009-09-15 | Tunney Timothy T | Method and apparatus for testing roof edge components |
| US20140090479A1 (en) * | 2012-09-28 | 2014-04-03 | Airbus Operations Gmbh | Test method, test rigs and control system |
| US9354149B2 (en) * | 2012-09-28 | 2016-05-31 | Airbus Operations Gmbh | Test method, test rigs and control system |
| CN110595901A (en) * | 2019-09-29 | 2019-12-20 | 扬州大学 | A new truss joint self-balancing test device and its test method |
| CN110595901B (en) * | 2019-09-29 | 2022-04-12 | 扬州大学 | A new type of self-balancing test device for truss joints and its test method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: XENEX CORPORATION OF NEVADA, A NE CORP. Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:KELLER, JAMES R.;REEL/FRAME:003942/0109 Effective date: 19800729 Owner name: XENEX CORPORATION OF NEVADA, A CORP., NEBRASKA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:KELLER, JAMES R.;REEL/FRAME:003942/0109 Effective date: 19800729 |
|
| AS | Assignment |
Owner name: ZIONS FIRST NATIONAL BANK, SALT LAKE CITY, UTAH, A Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:XENEX CORPORATION;REEL/FRAME:004145/0437 Effective date: 19830623 Owner name: ZIONS FIRST NATIONAL BANK, SALT LAKE CITY, UTAH, A Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:XENEX CORPORATION;REEL/FRAME:004145/0437 Effective date: 19830623 |
|
| AS | Assignment |
Owner name: ZIONS FIRST NATIONAL BANK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:XENEX CORPORATION OF NEVADA;REEL/FRAME:004150/0317 Effective date: 19811023 |
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| STCF | Information on status: patent grant |
Free format text: PATENTED FILE - (OLD CASE ADDED FOR FILE TRACKING PURPOSES) |
|
| AS | Assignment |
Owner name: GEORGIA-PACIFIC CORPORATION, A GA CORP. Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:ZIONS FIRST NATIONAL BANK;REEL/FRAME:004928/0383 Effective date: 19880726 Owner name: GEORGIA-PACIFIC CORPORATION, A GA CORP. Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:HATFIELD, THOMAS K., TRUSTEE;REEL/FRAME:004928/0365 Effective date: 19880620 |